CN213677214U - Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon - Google Patents
Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon Download PDFInfo
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- CN213677214U CN213677214U CN202021859950.7U CN202021859950U CN213677214U CN 213677214 U CN213677214 U CN 213677214U CN 202021859950 U CN202021859950 U CN 202021859950U CN 213677214 U CN213677214 U CN 213677214U
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Abstract
The utility model discloses an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon, include: the automatic weapon transport device comprises a connecting hinge I, a weapon fixing support, a mechanical arm, a control bogie, a chassis, a weapon transport box body, a connecting hinge II and a wheel assembly; the wheel assembly is arranged below the chassis, so that the driving of the integrated vehicle for transporting and loading the missile of the airborne weapon of the unmanned aerial vehicle is realized; the control bogie and the weapon transportation box body are arranged above the chassis; wherein the control bogie is positioned in front of the weapon transport box body; one end of the mechanical arm is installed on the chassis through a connecting hinge II, and the other end of the mechanical arm is connected with the weapon fixing support through a connecting hinge I. Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon, reduced the vibration in the unmanned aerial vehicle airborne weapon transportation, reduced workman intensity of labour, improved the efficiency of unmanned aerial vehicle carried weapon.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon.
Background
The existing scouting and hitting integrated unmanned aerial vehicle is long in carrying distance before carrying out tasks, airborne weapons are transported to a working area by an ammunition warehouse, the airborne weapons generate large and lasting vibration, the integral structure and internal precision equipment of the airborne weapons are prone to vibration damage, the performance and reliability of the airborne weapons are greatly influenced, the airborne weapons carrying process of the unmanned aerial vehicle adopts manual carrying to carry out a fixing mode, the working strength is high, and the carrying efficiency is low.
SUMMERY OF THE UTILITY MODEL
The technical problem of the utility model is solved: the defects of the prior art are overcome, the integrated carrier for the unmanned aerial vehicle airborne weapon transportation hanging bomb is provided, the vibration in the transportation process of the unmanned aerial vehicle airborne weapon is reduced, the labor intensity of workers is reduced, and the efficiency of the unmanned aerial vehicle airborne weapon is improved.
In order to solve the technical problem, the utility model discloses an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon, include: the automatic weapon transport device comprises a connecting hinge I, a weapon fixing support, a mechanical arm, a control bogie, a chassis, a weapon transport box body, a connecting hinge II and a wheel assembly;
the wheel assembly is arranged below the chassis, so that the driving of the integrated vehicle for transporting and loading the missile of the airborne weapon of the unmanned aerial vehicle is realized;
the control bogie and the weapon transportation box body are arranged above the chassis; wherein the control bogie is positioned in front of the weapon transport box body;
one end of the mechanical arm is mounted on the chassis through a connecting hinge II, and the other end of the mechanical arm is connected with the weapon fixing support through a connecting hinge I; wherein, the connecting hinge II is positioned in front of the control bogie.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, the weapon fixed bolster includes: a support bucket, a weapon fixing groove and a detachable weapon fixing belt;
the supporting hopper is hinged with the other end of the mechanical arm through a connecting hinge I;
a plurality of weapon fixing grooves are uniformly distributed on the opening section of the side edge of the supporting bucket;
the two ends of the detachable weapon fixing ribbon are detachably connected with the weapon fixing grooves respectively.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, at the carry in-process of weapon, fix the weapon in the weapon fixed slot to use and to dismantle the fastening of weapon fixing ribbon.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, the arm includes: the mechanical arm comprises an end section hydraulic device, a mechanical arm end section, an end section hydraulic device I, a connecting hinge III, an end section hydraulic device II and a mechanical arm end section;
one end of the mechanical arm end section is hinged with the supporting bucket through a connecting hinge I, and the other end of the mechanical arm end section is hinged with one end of the mechanical arm root section through a connecting hinge III; the other end of the mechanical arm root section is hinged with the chassis through a connecting hinge II;
one end of the end section hydraulic device is fixed on the end section of the mechanical arm, and the other end of the end section hydraulic device is connected with the supporting hopper and used for realizing hydraulic drive control on the supporting hopper, so that the supporting hopper can rotate around the connecting hinge I;
one end of the root section hydraulic device II is fixed on the chassis, and the other end of the root section hydraulic device II is connected with the mechanical arm root section and used for realizing hydraulic drive control on the mechanical arm root section so that the mechanical arm root section can rotate around the connecting hinge II;
one end of the root section hydraulic device I is fixed on the root section of the mechanical arm, and the other end of the root section hydraulic device I is connected with the end section of the mechanical arm and used for realizing hydraulic drive control on the end section of the mechanical arm, so that the end section of the mechanical arm can rotate around the connecting hinge III.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, the control bogie includes: a cab and a steering mechanism;
the cab and the steering mechanism are respectively arranged above the chassis;
and a controller is arranged in the cab, and controls the rotation of the steering mechanism and the hydraulic driving control of the end section hydraulic device, the root section hydraulic device I and the root section hydraulic device II through the controller.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, the control of arm includes: the up-and-down motion of the mechanical arm root section is controlled through the root section hydraulic device II, the up-and-down motion of the mechanical arm end section is controlled through the root section hydraulic device I, and the pitching motion of the weapon fixing support is controlled through the end section hydraulic device, so that the requirements of mounting positions and angles of various weapons are met.
In the integrated vehicle for transporting and hanging the weapon on the aircraft of the unmanned aerial vehicle, when the weapon is loaded and unloaded, the support bucket of the weapon fixing support is moved into the weapon transport box body by controlling the steering of the steering mechanism, the lifting of the mechanical arm and the movement of the weapon fixing support, and the weapon in the weapon transport box body is fixed into the weapon fixing groove.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, the chassis includes: a tractor chassis and a trailer chassis;
the traction chassis is connected with the trailer chassis through a connecting mechanism;
the control bogie is arranged on the traction chassis;
the weapon transport box body is arranged on the trailer chassis.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, weapon transport box includes: the side baffle, the front baffle, the box body, the rear baffle and the fixing buckle;
the front baffle, the two side baffles and the rear baffle are respectively connected with the box body and are positioned in the front, left, right and rear directions of the box body;
the front baffle is vertically and fixedly arranged in front of the box body, the side baffle can rotate around the connecting axis of the side baffle and the box body, and the rear baffle can rotate around the connecting axis of the rear baffle and the box body;
when the two side baffles and the rear baffle rotate to vertical positions, the two side baffles and the rear baffle are fixed through the fixing buckles.
In the integrative car of bullet is hung in the transport of above-mentioned unmanned aerial vehicle airborne weapon, still include: a bumper;
the bumper is installed at the front end of the chassis.
The utility model has the advantages of it is following:
(1) the utility model discloses an integrated vehicle for transporting and hanging ammunition of an unmanned aerial vehicle airborne weapon, which reduces the vibration in the transportation process of the airborne weapon, reduces the labor intensity of workers and improves the transportation efficiency of the airborne weapon; novel reasonable, the flexible operation of structural design, removal are convenient.
(2) The utility model discloses an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon, through the arm that can free rotation's control bogie and free lift, realized that the high efficiency of airborne ammunition swiftly shifts to under the stores pylon from the transport vechicle to can accurate control carry position and angle, realize the quick loading and the carry of unmanned aerial vehicle ammunition, remove the tired of traditional ground service manual work carry from, and can carry the ammunition of bigger weight.
(3) The utility model discloses an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon, through the control bogie of horizontal direction and the arm of vertical direction to and the motion of a plurality of degrees of freedom of every single move adjustable weapon fixed bolster realization airborne weapon, the alignment work before the weapon carry of being convenient for.
Drawings
Fig. 1 is a schematic right front side view of an integrated transportation and missile hanging vehicle for an airborne weapon of an unmanned aerial vehicle in an embodiment of the invention;
fig. 2 is the embodiment of the utility model provides an in the embodiment of the utility model provides a rear left side schematic diagram of integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the embodiments of the present invention will be described in further detail with reference to the accompanying drawings.
According to fig. 1-2, in this embodiment, this integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon includes: the mechanical arm comprises a connecting hinge I4, a weapon fixing bracket 5, a mechanical arm 6, a control bogie 12, a chassis 14, a weapon transportation box body 15, a connecting hinge II 18 and a wheel assembly 27. The wheel assembly 27 is arranged below the chassis 14, so that the integrated vehicle for transporting and loading the missile of the airborne weapon of the unmanned aerial vehicle is driven; the control bogie 12 and the weapon transport box 15 are installed above the chassis 14, and the control bogie 12 is positioned in front of the weapon transport box 15; one end of the mechanical arm 6 is mounted on the chassis 14 through a connecting hinge II 18, and the other end of the mechanical arm is connected with the weapon fixing bracket 5 through a connecting hinge I4; wherein the connecting joint ii 18 is located in front of the control bogie 12.
In this embodiment, the weapon fixing bracket 5 may specifically include: a support bucket 1, a weapon securing slot 2 and a detachable weapon securing strap 3. Wherein, the supporting bucket 1 is hinged with the other end of the mechanical arm 6 through a connecting hinge I4; a plurality of weapon fixing grooves 2 are uniformly distributed on the opening section of the side edge of the supporting bucket 1; the two ends of the detachable weapon fixing ribbon 3 are detachably connected with the weapon fixing grooves 2 respectively.
Preferably, during the mounting of the weapon, the weapon is secured in the weapon securing slot 2 and fastened using a removable weapon securing strap 3.
In this embodiment, the robot arm 6 may specifically include: the device comprises a section hydraulic device 7, a mechanical arm root section 8, a root section hydraulic device I9, a connecting hinge III 10, a root section hydraulic device II 11 and a mechanical arm section 28. One end of the mechanical arm end section 28 is hinged with the support bucket 1 through a connecting hinge I4, and the other end of the mechanical arm end section 28 is hinged with one end of the mechanical arm root section 8 through a connecting hinge III 10; the other end of the mechanical arm root section 8 is hinged with the chassis 14 through a connecting hinge II 18; one end of the end section hydraulic device 7 is fixed on the mechanical arm end section 28, and the other end of the end section hydraulic device is connected with the supporting bucket 1 and used for realizing hydraulic drive control on the supporting bucket 1, so that the supporting bucket 1 can rotate around the connecting hinge I4; one end of the root section hydraulic device II 11 is fixed on the chassis 14, and the other end of the root section hydraulic device II is connected with the mechanical arm root section 8, so that hydraulic drive control over the mechanical arm root section 8 is realized, and the mechanical arm root section 8 can rotate around the connecting hinge II 18; one end of the end section hydraulic device I9 is fixed on the mechanical arm end section 8, and the other end is connected with the mechanical arm end section 28, so that hydraulic drive control of the mechanical arm end section 28 is realized, and the mechanical arm end section 28 can rotate around the connecting hinge III 10.
Preferably, the control of the robot arm 6 may specifically include: the up-and-down movement of the mechanical arm root section 8 is controlled through the root section hydraulic device II 11, the up-and-down movement of the mechanical arm end section 28 is controlled through the root section hydraulic device I9, and the pitching movement of the weapon fixing support 5 is controlled through the end section hydraulic device 7, so that the requirements of mounting positions and angles of various weapons are met.
In this embodiment, the control bogie 12 may specifically include: a cab 16 and a steering mechanism 17. Wherein, the cab 16 and the steering mechanism 17 are respectively arranged above the chassis 14; a controller is arranged in the cab 16, and the controller controls the rotation of the steering mechanism 17 and the hydraulic driving control of the end section hydraulic device 7, the root section hydraulic device I9 and the root section hydraulic device II 11.
Preferably, when loading and unloading the weapon, the support bucket 1 of the weapon fixing bracket 5 is moved into the weapon transport box 15 and the weapon in the weapon transport box 15 is fixed to the weapon fixing groove 2 by controlling the steering of the steering mechanism 17, the raising and lowering of the robot arm 6, and the movement of the weapon fixing bracket 5.
In this embodiment, the chassis 14 mainly plays a role of long-distance transportation and shock absorption, and specifically may include: a tractor chassis 25 and a trailer chassis 26. Wherein, the traction chassis 25 is connected with the trailer chassis 26 through a connecting mechanism; the control bogie 12 is mounted on a traction chassis 25; the weapons transport pod 15 is mounted on the trailer chassis 26.
In this embodiment, the weapon transport case 15 may specifically include: side shield 20, front shield 21, box 22, back shield 23 and fixing buckle 24. The front baffle 21, the two side baffles 20 and the rear baffle 23 are respectively connected with the box body 22 and are positioned in the front, left, right and rear directions of the box body 22; the front baffle 21 is vertically and fixedly arranged in front of the box body 22, the side baffle 20 can rotate around the connecting axis of the side baffle 20 and the box body 22, and the rear baffle 23 can rotate around the connecting axis of the rear baffle 23 and the box body 22; when the two side guards 20 and the back guard 23 are rotated to the vertical position, the two side guards 20 and the back guard 23 are fixed by the fixing buckles 24. It can be seen that in this embodiment, the two side guards 20 and the tailgate 23 can be lowered to facilitate transport of the weapon and secured by the securing clip 24.
In this embodiment, this integrative car of on-board weapon transport of unmanned aerial vehicle string bullet can also include: a bumper 13. Wherein, bumper 13 is installed at the front end of chassis 14, has improved the security of the integrative car of bullet is hung in the transport of unmanned aerial vehicle airborne weapon.
On the basis of the above embodiments, the following description is made in conjunction with the working principle of the integrated transportation and missile loading vehicle for the airborne weapons of the unmanned aerial vehicle.
In this embodiment, the specific workflow of this integrative car of airborne weapon transport of unmanned aerial vehicle string bullet when transportation and string bullet is as follows:
step 1, the fixing buckle 24 is loosened, the two side guards 20 and the rear guard 23 are put down, and the airborne weapon and the bracket thereof are fixed in the box body 22.
Step 2, the two side baffles 20 and the rear baffle 23 are folded, and the fixing buckle 24 is locked; the operator maneuvers the vehicle at the cockpit 16 to transport the on-board weapons from the magazine to the ammunition loading site.
And 3, after the cartridge transports the airborne weapon to the ammunition mounting place, an operator controls the control bogie 12, turns the mechanical arm 6 to the weapon transport box body 15, places the airborne weapon in the weapon fixing groove 2 and fixes the airborne weapon by using the detachable weapon fixing belt 3.
And 4, controlling the mechanical arm root section 8 and the mechanical arm end section 28 to move up and down by driving the root section hydraulic device I9 and the root section hydraulic device II 11 by an operator, controlling the pitching motion of the weapon fixing support 5 by the end section hydraulic device 7, moving the airborne weapon to a proper hanging point of the unmanned aerial vehicle by controlling the bogie 12, loosening the detachable weapon fixing tie 3, and hanging the weapon on the unmanned aerial vehicle hanger.
Although the present invention has been disclosed in the preferred embodiments, it is not intended to limit the present invention, and any person skilled in the art can use the above-mentioned method and technical contents to make possible changes and modifications to the technical solution of the present invention without departing from the spirit and scope of the present invention, therefore, any simple modification, equivalent changes and modifications made to the above embodiments by the technical substance of the present invention all belong to the protection scope of the technical solution of the present invention.
The details of the present invention not described in detail in the specification are well known to those skilled in the art.
Claims (10)
1. The utility model provides an integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon which characterized in that includes: the automatic weapon transport device comprises a connecting hinge I (4), a weapon fixing support (5), a mechanical arm (6), a control bogie (12), a chassis (14), a weapon transport box body (15), a connecting hinge II (18) and a wheel assembly (27);
the wheel assembly (27) is arranged below the chassis (14) to drive the integrated transportation and missile hanging vehicle of the airborne weapon of the unmanned aerial vehicle;
the control bogie (12) and the weapon transport box body (15) are arranged above the chassis (14); wherein the control bogie (12) is located in front of the weapon transport box (15);
one end of the mechanical arm (6) is arranged on the chassis (14) through a connecting hinge II (18), and the other end of the mechanical arm is connected with the weapon fixing support (5) through a connecting hinge I (4); wherein the connecting hinge II (18) is positioned in front of the control bogie (12).
2. The integrated vehicle for the transport and loading of airborne weapons of unmanned aerial vehicle of claim 1 wherein the weapon mount (5) comprises: the support bucket (1), the weapon fixing groove (2) and the detachable weapon fixing bandage (3);
the supporting hopper (1) is hinged with the other end of the mechanical arm (6) through a connecting hinge I (4);
a plurality of weapon fixing grooves (2) are uniformly distributed on the opening section of the side edge of the supporting bucket (1);
two ends of the detachable weapon fixing bandage (3) are respectively detachably connected with the weapon fixing groove (2).
3. The integrated vehicle for the transportation and the loading of the weapon on the aircraft of unmanned aerial vehicle according to claim 2, characterized in that during the loading of the weapon, the weapon is fixed in the weapon fixing slot (2) and fastened with a detachable weapon fixing tie (3).
4. The integrated vehicle for the transport and loading of airborne weapons of unmanned aerial vehicle of claim 2 wherein the robotic arm (6) comprises: the robot comprises a section hydraulic device (7), a mechanical arm root section (8), a root section hydraulic device I (9), a connecting hinge III (10), a root section hydraulic device II (11) and a mechanical arm section (28);
one end of the mechanical arm end section (28) is hinged with the supporting bucket (1) through a connecting hinge I (4), and the other end of the mechanical arm end section is hinged with one end of the mechanical arm root section (8) through a connecting hinge III (10); the other end of the mechanical arm root section (8) is hinged with the chassis (14) through a connecting hinge II (18);
one end of the end section hydraulic device (7) is fixed on the end section (28) of the mechanical arm, and the other end of the end section hydraulic device is connected with the supporting bucket (1) and used for realizing hydraulic drive control on the supporting bucket (1) so that the supporting bucket (1) can rotate around the connecting hinge I (4);
one end of the root section hydraulic device II (11) is fixed on the chassis (14), and the other end of the root section hydraulic device II is connected with the mechanical arm root section (8) and used for realizing hydraulic drive control on the mechanical arm root section (8) so that the mechanical arm root section (8) can rotate around the connecting hinge II (18);
one end of the root section hydraulic device I (9) is fixed on the mechanical arm root section (8), and the other end of the root section hydraulic device I is connected with the mechanical arm end section (28) and used for realizing hydraulic drive control on the mechanical arm end section (28) so that the mechanical arm end section (28) can rotate around the connecting hinge III (10).
5. The integrated vehicle for the transport and loading of airborne weapons of unmanned aerial vehicle of claim 4 wherein the control bogie (12) comprises: a cab (16) and a steering mechanism (17);
the cab (16) and the steering mechanism (17) are respectively arranged above the chassis (14);
a controller is arranged in the cab (16), and controls the rotation of the steering mechanism (17) and the hydraulic driving control of the end section hydraulic device (7), the root section hydraulic device I (9) and the root section hydraulic device II (11) through the controller.
6. The integrated vehicle for the transport and loading of airborne weapons of unmanned aerial vehicle of claim 5 wherein the control of the robotic arm (6) includes: the up-and-down motion of the mechanical arm root section (8) is controlled through the root section hydraulic device II (11), the up-and-down motion of the mechanical arm end section (28) is controlled through the root section hydraulic device I (9), and the pitching motion of the weapon fixing support (5) is controlled through the end section hydraulic device (7), so that the requirements of the mounting positions and angles of various weapons are met.
7. The integrated vehicle for transporting and loading weapons on board an unmanned aerial vehicle of claim 6 wherein, when loading and unloading weapons, the support bucket (1) of the weapon fixing bracket (5) is moved into the weapon transport box (15) by controlling the steering of the steering mechanism (17), the lifting and lowering of the mechanical arm (6), and the movement of the weapon fixing bracket (5), and the weapons in the weapon transport box (15) are fixed in the weapon fixing slot (2).
8. The integrated vehicle for the transport and loading of weapons onboard an unmanned aerial vehicle of claim 1, wherein the chassis (14) comprises: a towing chassis (25) and a trailer chassis (26);
the traction chassis (25) is connected with the trailer chassis (26) through a connecting mechanism;
the control bogie (12) is arranged on a traction chassis (25);
the weapon transport box (15) is mounted on a trailer chassis (26).
9. The integrated vehicle for the on-board weapon transport and ammunition loading of an unmanned aerial vehicle of claim 8, characterized in that the weapon transport box (15) comprises: the side baffle (20), the front baffle (21), the box body (22), the rear baffle (23) and the fixing buckle (24);
the front baffle (21), the two side baffles (20) and the rear baffle (23) are respectively connected with the box body (22) and are positioned in the front, left, right and rear directions of the box body (22);
the front baffle (21) is vertically and fixedly arranged in front of the box body (22), the side baffle (20) can rotate around the connecting axis of the side baffle (20) and the box body (22), and the rear baffle (23) can rotate around the connecting axis of the rear baffle (23) and the box body (22);
when the two side baffles (20) and the rear baffle (23) rotate to the vertical position, the two side baffles (20) and the rear baffle (23) are fixed through the fixing buckles (24).
10. The integrated transport and missile loading vehicle for the airborne weapons of the unmanned aerial vehicle of claim 1, further comprising: a bumper (13);
the bumper (13) is mounted on the front end of the chassis (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021859950.7U CN213677214U (en) | 2020-08-31 | 2020-08-31 | Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021859950.7U CN213677214U (en) | 2020-08-31 | 2020-08-31 | Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213677214U true CN213677214U (en) | 2021-07-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021859950.7U Active CN213677214U (en) | 2020-08-31 | 2020-08-31 | Integrative car of bullet is hung in transportation of unmanned aerial vehicle airborne weapon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213677214U (en) |
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2020
- 2020-08-31 CN CN202021859950.7U patent/CN213677214U/en active Active
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